Source/Vortex Panel Method: Airfoil 

The source/vortex panel method code in this video is a combination of the source and vortex panel methods that I have used in my previous videos. This code solves some of the problems that were mentioned in my "Vortex Panel Method: Airfoil" video.
In this penultimate video of my Panel Methods series, we will look at how to populate the matrix system to obtain the solution of the source and vortex strengths. Then we'll go through a bunch of examples of different airfoils to see how well this method works. Comparisons of the lift coefficient, moment coefficient, and pressure coefficient to XFOIL will be made.
In the next (and last) video of this series, we will update this code to be able to work with any number of airfoils.
===== CODE =====
► My website
www.joshtheengi...
► GitHub
github.com/jte...
===== RELEVANT VIDEOS =====
► Panel Methods Playlist
• How To: Run XFoil from...
► Source Panel Method: Airfoil
• Source Panel Method: A...
► Vortex Panel Method: Airfoil
• Vortex Panel Method: A...
► Source/Vortex Panel Method: System of Equations
• Source/Vortex Panel Me...
===== NOTES =====
→ The code is also available in Python, but I didn't include it in this video.
→ The streamline computation section in the Python code takes a really long time to run in comparison to the same MATLAB code. I'm assuming it has to do with the external function calls taking longer, but if you have any suggestions on speeding up that aspect of the code, please let me know.
===== ERRORS =====
→ If you see an error in the video, please let me know and I will include it here.
===== REFERENCES =====
Note: the links are Amazon affiliate links. If you do happen to want to buy the book and use the link below, it helps me out a little.
► Fundamentals of Aerodynamics, Anderson
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► Foundations of Aerodynamics, Kuethe and Chow
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► Theory of Wing Sections, Abbott and Doenhoff
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